Question: Consider a shock wave moving through air at 2 9 3 K and 1 atm. Immediately downstream ( behind ) the shock wave, the air
Consider a shock wave moving through air at K and atm. Immediately downstream behind the shock wave, the air temperature and pressure increase to K and atm. Calculate the changes in the following quantities across the wave show details of your calculation:
a Enthalpy
b Internal energy
c Entropy
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